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时间:2011-03-27 08:44来源:蓝天飞行翻译 作者:admin
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R R R  (1) Apply masking paper or masking tape BONDING AND ADHESIVE COMPOUNDS (Material No. 08-074) on the equipment and fittings adjacent to the area.
 (2) Apply a layer of STORAGE PRESERVATION (Material No. 15-005) or STORAGE PRESERVATION (Material No. 15-006) to the inspected area.
 (3) Remove the masking paper or the masking tape.
 5. Close-up________
 Subtask 53-11-00-410-072
 A. Close Access
 (1) Close the aft nose-gear doors 715 and 716.
 (2) Make sure that the work area is clean and clear of tool(s) and other items.
 (3) Remove the access platform(s).

 CES


 TASK 53-11-00-210-032 
R R  Detailed Inspection of Fuselage Skin, between FR 21 and FR 23 LH and FR 17 and FR 18 RH, from Stringer 31 to Stringer 36
 1. Reason for the Job__________________
 Refer to the MPD TASK: 531172-01
 2. Job Set-up Information______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific  access platform 1.50 m (4 ft. 11 in.)
 B. Consumable Materials
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
Material No. 11-004 Material No. 19-003  USA MIL-T-81533 1.1.1TRICHLOROETHANE (METHYL CHLOROFORM) (Ref. 20-31-00)USA AMS 3819 LINT-FREE COTTON CLOTH (Ref. 20-31-00)
 C. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R  SRM 511100 P.Block 001 SRM 512200 P.Block 001 53-11-00-991-035 53-11-00-991-034  (for corrective action)(for corrective action) Fig. 640 Fig. 641

 

 3. Job Set-up__________
 Subtask 53-11-00-941-080 
R  A. Put an access platform in position: - for the left side: at the zone 127, - for the right side: at the zone 126.
 Subtask 53-11-00-110-080
 B. Cleaning of the Structure
 WARNING : USE SOLVENTS/CLEANING AGENTS, SEALANTS AND OTHER SPECIAL_______ MATERIALS ONLY WITH A GOOD SUPPLY OF AIR. OBEY THE MANUFACTURERS INSTRUCTIONS. PUT ON PROTECTIVE CLOTHING. DO NOT GET THEM IN YOUR MOUTH. DO NOT SMOKE. DO NOT BREATHE THE GAS. THESE MATERIALS ARE POISONOUS, FLAMMABLE AND SKIN IRRITANT. GET MEDICAL HELP IF YOUR SKIN OR EYES BECOME IRRITATED.
 WARNING : OBEY THE MANUFACTURER'S INSTRUCTIONS WHEN YOU USE THIS/THESE_______ MATERIAL/S. USE PROTECTIVE CLOTHING, RUBBER GLOVES, GOGGLES AND A MASK. 
R R R  (1) Clean the inspection area with CLEANING AGENTS (Material No. 11-004) and a lint-free cotton cloth MISCELLANEOUS (Material No. 19-003), if necessary.
 4. Procedure_________
 Subtask 53-11-00-220-088
 A. Inspection 
R R R  (1) Do a detailed inspection of the structure of the fuselage skin: - for the left side: from FR21 to FR23 between STGR31 and STGR36. (Ref. Fig. 640/TASK 53-11-00-991-035) - for the right side: from FR17 to FR18 between the STGR31 and STGR36. (Ref. Fig. 641/TASK 53-11-00-991-034)

 CES


R R  Fuselage Skin Between FR21 and FR23, Left Side, from STGR31 to STGR36 Figure 640/TASK 53-11-00-991-035
 EFF :  ALL  53-11-00 Page A659 Aug 01/03
 CES 

 

R R  Fuselage Skin between FR17 and FR18, Right Side, from STGR31 to STGR36 Figure 641/TASK 53-11-00-991-034
 EFF :  ALL  53-11-00 Page A660 Aug 01/03
 CES 

 

 (2) Make sure that there is no:

R R  (a) corrosion damage: - If you find corrosion damage, refer to the Structural Repair Manual (Ref. SRM 512200 P.Block 001) for types, inspection, removal and corrosion protection.
R R R  (b) other damage (cracks, scratches, stress, marks, dents, bumps,...): - If you find other damage, refer to the Structural Repair Manual (Ref. SRM 511100 P.Block 001) for damage classification and corrective action.
 5. Close-up________
 Subtask 53-11-00-942-088
 A. Close Access
 (1) Make sure that the work area is clean and clear of tool(s) and other items.
 (2) Remove the access platform(s).

 

 TASK 53-11-00-210-040 
R  Detailed Inspection of Forward Face of Front Pressure Bulkhead Attached to FR 1
 1. Reason for the Job__________________
 Refer to the MPD TASK: 531175-01
 2. Job Set-up Information______________________ 
 
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